Review Article
A Review on Vertical Take-Off and Landing (VTOL) Tilt-Rotor and Tilt Wing Unmanned Aerial Vehicles (UAVs)
Table 8
Prototyping analysis done by various teams.
| Team | Innovation carried | Software/technique used | Remarks |
| B. V. Sandilya | Tilt quad rotor aircraft have features of both fixed-wing UAV | 3D modeling | Further need to control the UAV using a fully autonomous system is required for a more efficient | Seunghee Yu | Lighter than Tr-100 and has easy manoeuvrability | Prototype built | Summarizes a comparison report in terms of performance and applications | D. F. Finger | Balancing electric propulsion system | Tool by institute of aircraft engineering of FH aachen | Fully electric aircraft are still too heavy and hybrid electric provide no clear advantage over other systems | D.F Finger | Various configurations are tested with different forward and vertical motors | 3D modeling | VTOL aircraft are certainly very feasible; their design remains challenging, but the advantages are still highly beneficial |
|
|